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GOE 460 AIRFOIL (goe460-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 460 AIRFOIL (goe460-il)
Reynolds number: 200,000
Max Cl/Cd: 46.41 at α=9.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe460-il-200000.txt
Download as CSV file: xf-goe460-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 460 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0724   0.08839   0.08230  -0.0636   1.0000   0.0791
 -19.500  -1.0727   0.08546   0.07932  -0.0645   1.0000   0.0807
 -19.250  -1.0790   0.08173   0.07547  -0.0657   1.0000   0.0825
 -19.000  -1.0890   0.07759   0.07114  -0.0670   1.0000   0.0841
 -18.750  -1.0896   0.07481   0.06829  -0.0675   1.0000   0.0859
 -18.500  -1.0830   0.07297   0.06650  -0.0676   1.0000   0.0878
 -18.250  -1.0833   0.07026   0.06374  -0.0681   1.0000   0.0900
 -18.000  -1.0876   0.06712   0.06046  -0.0687   1.0000   0.0921
 -17.750  -1.0953   0.06366   0.05680  -0.0692   1.0000   0.0941
 -17.500  -1.0833   0.06257   0.05584  -0.0687   1.0000   0.0967
 -17.250  -1.0813   0.06033   0.05357  -0.0687   1.0000   0.0995
 -17.000  -1.0839   0.05762   0.05073  -0.0687   1.0000   0.1023
 -16.750  -1.0804   0.05564   0.04874  -0.0683   1.0000   0.1055
 -16.500  -1.0767   0.05377   0.04691  -0.0678   1.0000   0.1090
 -16.250  -1.0783   0.05135   0.04439  -0.0675   1.0000   0.1128
 -16.000  -1.0746   0.04954   0.04263  -0.0667   1.0000   0.1171
 -15.750  -1.0742   0.04750   0.04059  -0.0660   1.0000   0.1215
 -15.500  -1.0763   0.04525   0.03822  -0.0652   1.0000   0.1262
 -15.250  -1.0739   0.04354   0.03665  -0.0642   1.0000   0.1312
 -15.000  -1.0752   0.04156   0.03458  -0.0631   1.0000   0.1364
 -14.750  -1.0743   0.03986   0.03295  -0.0618   1.0000   0.1413
 -14.500  -1.0745   0.03820   0.03126  -0.0604   1.0000   0.1464
 -14.250  -1.0737   0.03667   0.02966  -0.0588   1.0000   0.1516
 -14.000  -1.0731   0.03530   0.02834  -0.0570   1.0000   0.1562
 -13.750  -1.0724   0.03402   0.02698  -0.0550   1.0000   0.1615
 -13.500  -1.0702   0.03288   0.02583  -0.0529   1.0000   0.1662
 -13.250  -1.0687   0.03185   0.02480  -0.0505   1.0000   0.1707
 -13.000  -1.0681   0.03088   0.02373  -0.0479   1.0000   0.1759
 -12.750  -1.0658   0.02999   0.02283  -0.0452   1.0000   0.1805
 -12.500  -1.0649   0.02920   0.02206  -0.0422   1.0000   0.1850
 -12.250  -1.0662   0.02846   0.02125  -0.0388   1.0000   0.1902
 -12.000  -1.0658   0.02775   0.02050  -0.0353   1.0000   0.1951
 -11.750  -1.0659   0.02714   0.01993  -0.0317   1.0000   0.1998
 -11.500  -1.0693   0.02659   0.01933  -0.0275   1.0000   0.2049
 -11.250  -1.0745   0.02608   0.01872  -0.0228   1.0000   0.2098
 -11.000  -1.0744   0.02555   0.01830  -0.0189   1.0000   0.2150
 -10.750  -1.0808   0.02516   0.01788  -0.0139   1.0000   0.2200
 -10.500  -1.0901   0.02484   0.01745  -0.0083   1.0000   0.2248
 -10.250  -1.0908   0.02438   0.01708  -0.0041   1.0000   0.2301
 -10.000  -1.0968   0.02407   0.01676   0.0011   1.0000   0.2350
  -9.750  -1.1053   0.02384   0.01644   0.0068   1.0000   0.2401
  -9.500  -1.0789   0.02337   0.01603   0.0060   0.9962   0.2487
  -9.250  -1.0501   0.02314   0.01572   0.0048   0.9914   0.2577
  -9.000  -1.0226   0.02266   0.01531   0.0040   0.9859   0.2659
  -8.750  -0.9938   0.02244   0.01502   0.0030   0.9807   0.2751
  -8.500  -0.9642   0.02205   0.01469   0.0019   0.9758   0.2834
  -8.250  -0.9392   0.02178   0.01438   0.0018   0.9691   0.2918
  -8.000  -0.9029   0.02141   0.01405  -0.0005   0.9654   0.3004
  -7.750  -0.8807   0.02111   0.01376   0.0001   0.9581   0.3079
  -7.500  -0.8481   0.02074   0.01338  -0.0012   0.9526   0.3161
  -7.250  -0.8091   0.02037   0.01305  -0.0039   0.9493   0.3258
  -7.000  -0.7902   0.02005   0.01274  -0.0025   0.9404   0.3341
  -6.750  -0.7565   0.01966   0.01240  -0.0039   0.9353   0.3456
  -6.500  -0.7169   0.01919   0.01201  -0.0065   0.9322   0.3585
  -6.250  -0.7025   0.01891   0.01174  -0.0041   0.9217   0.3705
  -6.000  -0.6676   0.01846   0.01133  -0.0056   0.9170   0.3873
  -5.750  -0.6274   0.01793   0.01088  -0.0082   0.9142   0.4065
  -5.500  -0.6162   0.01766   0.01069  -0.0049   0.9026   0.4205
  -5.250  -0.5778   0.01717   0.01026  -0.0070   0.8988   0.4388
  -5.000  -0.5345   0.01671   0.00986  -0.0100   0.8964   0.4573
  -4.750  -0.5214   0.01653   0.00973  -0.0069   0.8851   0.4706
  -4.500  -0.4852   0.01615   0.00937  -0.0084   0.8805   0.4874
  -4.250  -0.4456   0.01576   0.00900  -0.0105   0.8772   0.5040
  -4.000  -0.4316   0.01564   0.00891  -0.0075   0.8653   0.5162
  -3.750  -0.3944   0.01530   0.00861  -0.0091   0.8603   0.5301
  -3.500  -0.3703   0.01511   0.00840  -0.0081   0.8516   0.5427
  -3.250  -0.3407   0.01486   0.00818  -0.0081   0.8431   0.5545
  -3.000  -0.3005   0.01453   0.00785  -0.0103   0.8379   0.5664
  -2.750  -0.2859   0.01447   0.00778  -0.0074   0.8252   0.5770
  -2.500  -0.2469   0.01418   0.00751  -0.0093   0.8186   0.5879
  -2.250  -0.2318   0.01412   0.00741  -0.0066   0.8058   0.5988
  -2.000  -0.1934   0.01387   0.00720  -0.0084   0.7983   0.6095
  -1.750  -0.1785   0.01381   0.00711  -0.0056   0.7850   0.6206
  -1.500  -0.1452   0.01364   0.00698  -0.0063   0.7753   0.6314
  -1.250  -0.1239   0.01352   0.00685  -0.0047   0.7623   0.6427
  -1.000  -0.0994   0.01343   0.00679  -0.0037   0.7499   0.6540
  -0.750  -0.0699   0.01331   0.00665  -0.0037   0.7391   0.6653
  -0.500  -0.0522   0.01327   0.00662  -0.0014   0.7260   0.6779
  -0.250  -0.0225   0.01324   0.00662  -0.0014   0.7147   0.6895
   0.000   0.0000   0.01321   0.00659   0.0000   0.7022   0.7022
   0.250   0.0225   0.01324   0.00662   0.0014   0.6896   0.7147
   0.500   0.0521   0.01327   0.00662   0.0014   0.6778   0.7259
   0.750   0.0700   0.01331   0.00666   0.0037   0.6653   0.7392
   1.000   0.0993   0.01343   0.00679   0.0037   0.6541   0.7501
   1.250   0.1240   0.01352   0.00686   0.0047   0.6428   0.7624
   1.500   0.1451   0.01364   0.00698   0.0063   0.6313   0.7753
   1.750   0.1785   0.01381   0.00711   0.0056   0.6206   0.7850
   2.000   0.1933   0.01387   0.00719   0.0084   0.6095   0.7982
   2.250   0.2318   0.01412   0.00742   0.0066   0.5989   0.8058
   2.500   0.2470   0.01418   0.00751   0.0093   0.5880   0.8186
   2.750   0.2859   0.01447   0.00778   0.0074   0.5770   0.8252
   3.000   0.3006   0.01454   0.00785   0.0103   0.5664   0.8380
   3.250   0.3409   0.01487   0.00818   0.0081   0.5546   0.8431
   3.500   0.3703   0.01511   0.00839   0.0081   0.5427   0.8515
   3.750   0.3945   0.01530   0.00861   0.0090   0.5301   0.8604
   4.000   0.4318   0.01564   0.00891   0.0074   0.5165   0.8653
   4.250   0.4456   0.01576   0.00900   0.0105   0.5040   0.8772
   4.500   0.4852   0.01614   0.00937   0.0084   0.4873   0.8805
   4.750   0.5212   0.01652   0.00972   0.0070   0.4707   0.8851
   5.000   0.5347   0.01671   0.00986   0.0100   0.4574   0.8964
   5.250   0.5779   0.01717   0.01026   0.0070   0.4389   0.8988
   5.500   0.6161   0.01766   0.01069   0.0049   0.4205   0.9026
   5.750   0.6273   0.01793   0.01087   0.0082   0.4063   0.9142
   6.000   0.6675   0.01845   0.01132   0.0057   0.3872   0.9171
   6.250   0.7025   0.01891   0.01173   0.0041   0.3705   0.9218
   6.500   0.7170   0.01919   0.01201   0.0065   0.3585   0.9322
   6.750   0.7566   0.01965   0.01239   0.0039   0.3454   0.9354
   7.000   0.7905   0.02005   0.01274   0.0024   0.3341   0.9405
   7.250   0.8095   0.02036   0.01304   0.0038   0.3257   0.9493
   7.500   0.8484   0.02074   0.01338   0.0012   0.3161   0.9526
   7.750   0.8809   0.02111   0.01375  -0.0002   0.3079   0.9581
   8.000   0.9032   0.02140   0.01404   0.0004   0.3004   0.9654
   8.250   0.9396   0.02177   0.01438  -0.0019   0.2917   0.9691
   8.500   0.9646   0.02204   0.01468  -0.0020   0.2833   0.9758
   8.750   0.9943   0.02243   0.01502  -0.0031   0.2751   0.9808
   9.000   1.0231   0.02266   0.01530  -0.0041   0.2659   0.9859
   9.250   1.0499   0.02312   0.01571  -0.0048   0.2575   0.9915
   9.500   1.0793   0.02336   0.01602  -0.0061   0.2485   0.9963
   9.750   1.1054   0.02382   0.01643  -0.0068   0.2401   1.0000
  10.000   1.0967   0.02405   0.01674  -0.0011   0.2349   1.0000
  10.250   1.0907   0.02437   0.01706   0.0041   0.2300   1.0000
  10.500   1.0904   0.02483   0.01743   0.0082   0.2248   1.0000
  10.750   1.0806   0.02514   0.01786   0.0139   0.2199   1.0000
  11.000   1.0744   0.02553   0.01828   0.0189   0.2150   1.0000
  11.250   1.0745   0.02606   0.01870   0.0228   0.2098   1.0000
  11.500   1.0693   0.02657   0.01931   0.0275   0.2049   1.0000
  11.750   1.0660   0.02711   0.01990   0.0317   0.1998   1.0000
  12.000   1.0659   0.02773   0.02048   0.0353   0.1950   1.0000
  12.250   1.0659   0.02844   0.02123   0.0388   0.1900   1.0000
  12.500   1.0654   0.02917   0.02203   0.0422   0.1850   1.0000
  12.750   1.0661   0.02996   0.02280   0.0452   0.1804   1.0000
  13.000   1.0684   0.03085   0.02371   0.0479   0.1757   1.0000
  13.250   1.0695   0.03182   0.02476   0.0505   0.1707   1.0000
  13.500   1.0707   0.03286   0.02579   0.0528   0.1660   1.0000
  13.750   1.0729   0.03400   0.02696   0.0549   0.1613   1.0000
  14.000   1.0738   0.03526   0.02830   0.0569   0.1561   1.0000
  14.250   1.0749   0.03662   0.02960   0.0587   0.1515   1.0000
  14.500   1.0755   0.03816   0.03122   0.0603   0.1462   1.0000
  14.750   1.0756   0.03981   0.03288   0.0617   0.1413   1.0000
  15.000   1.0765   0.04151   0.03452   0.0630   0.1364   1.0000
  15.250   1.0754   0.04348   0.03659   0.0640   0.1311   1.0000
  15.500   1.0781   0.04516   0.03812   0.0651   0.1261   1.0000
  15.750   1.0760   0.04742   0.04051   0.0659   0.1214   1.0000
  16.000   1.0764   0.04947   0.04254   0.0665   0.1170   1.0000
  16.250   1.0804   0.05126   0.04429   0.0673   0.1127   1.0000
  16.500   1.0787   0.05368   0.04682   0.0676   0.1089   1.0000
  16.750   1.0825   0.05557   0.04866   0.0681   0.1055   1.0000
  17.000   1.0868   0.05747   0.05057   0.0685   0.1023   1.0000
  17.250   1.0836   0.06024   0.05348   0.0684   0.0994   1.0000
  17.500   1.0859   0.06245   0.05572   0.0685   0.0967   1.0000
  17.750   1.0988   0.06344   0.05656   0.0690   0.0939   1.0000
  18.000   1.0894   0.06711   0.06046   0.0684   0.0920   1.0000
  18.250   1.0853   0.07025   0.06372   0.0678   0.0898   1.0000
  18.500   1.0860   0.07284   0.06636   0.0673   0.0878   1.0000
  18.750   1.0925   0.07468   0.06816   0.0672   0.0858   1.0000
  19.000   1.0917   0.07752   0.07107   0.0667   0.0840   1.0000
  19.250   1.0816   0.08168   0.07542   0.0654   0.0824   1.0000
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